US7040082B2 - Assistance and emergency drive for electrically-driven accessories - Google Patents

Assistance and emergency drive for electrically-driven accessories Download PDF

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Publication number
US7040082B2
US7040082B2 US10/617,656 US61765603A US7040082B2 US 7040082 B2 US7040082 B2 US 7040082B2 US 61765603 A US61765603 A US 61765603A US 7040082 B2 US7040082 B2 US 7040082B2
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US
United States
Prior art keywords
electric motor
pump
air turbine
turboengine
air
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Expired - Lifetime, expires
Application number
US10/617,656
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English (en)
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US20040011018A1 (en
Inventor
Philippe Bouiller
Michel Franchet
Jean-Pierre Ruis
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA Moteurs SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SNECMA Moteurs SA filed Critical SNECMA Moteurs SA
Assigned to SNECMA MOTEURS reassignment SNECMA MOTEURS ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BOUILLER, PHILIPPE, FRANCHET, MICHEL, RUIS, JEAN-PIERRE
Publication of US20040011018A1 publication Critical patent/US20040011018A1/en
Application granted granted Critical
Publication of US7040082B2 publication Critical patent/US7040082B2/en
Assigned to SNECMA reassignment SNECMA CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: SNECMA MOTEURS
Assigned to SAFRAN AIRCRAFT ENGINES reassignment SAFRAN AIRCRAFT ENGINES CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: SNECMA
Assigned to SAFRAN AIRCRAFT ENGINES reassignment SAFRAN AIRCRAFT ENGINES CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Assignors: SNECMA
Adjusted expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32Arrangement, mounting, or driving, of auxiliaries
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/08Adaptations for driving, or combinations with, pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10Adaptations for driving, or combinations with, electric generators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
    • F02C6/04Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
US10/617,656 2002-07-17 2003-07-14 Assistance and emergency drive for electrically-driven accessories Expired - Lifetime US7040082B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0209028A FR2842564B1 (fr) 2002-07-17 2002-07-17 Assistance et secours a l'entrainement electrique d'accessoires dans un turbomoteur
FR0209028 2002-07-17

Publications (2)

Publication Number Publication Date
US20040011018A1 US20040011018A1 (en) 2004-01-22
US7040082B2 true US7040082B2 (en) 2006-05-09

Family

ID=29763898

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/617,656 Expired - Lifetime US7040082B2 (en) 2002-07-17 2003-07-14 Assistance and emergency drive for electrically-driven accessories

Country Status (8)

Country Link
US (1) US7040082B2 (fr)
EP (1) EP1382817B1 (fr)
JP (1) JP4115902B2 (fr)
CA (1) CA2434492C (fr)
DE (1) DE60304135T2 (fr)
FR (1) FR2842564B1 (fr)
RU (1) RU2321761C2 (fr)
UA (1) UA79084C2 (fr)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060137355A1 (en) * 2004-12-27 2006-06-29 Pratt & Whitney Canada Corp. Fan driven emergency generator
US20100003148A1 (en) * 2007-07-30 2010-01-07 Hispano Suiza Assistance and emergency backup for the electrical drive of a fuel pump in a turbine engine
US20100237619A1 (en) * 2006-09-12 2010-09-23 Josef Pozivil Power recovery machine
US20110181050A1 (en) * 2007-08-22 2011-07-28 General Electric Company Combustion turbine cooling media supply method
US20110303390A1 (en) * 2010-06-14 2011-12-15 Vykson Limited Combustion Chamber Cooling Method and System
US8519555B2 (en) 2010-11-29 2013-08-27 Pratt & Whitney Canada Corp. Combination low spool generator and ram air turbine generator
US20160053691A1 (en) * 2014-08-22 2016-02-25 Rolls-Royce Corporation Gas turbine engine system
US20180030900A1 (en) * 2016-08-01 2018-02-01 Honeywell International Inc. Air Turbine Starter with Integrated Motor for Main Engine Cooling
US20180093760A1 (en) * 2016-10-05 2018-04-05 Sikorsky Aircraft Corporation Flight control pump systems
US10914234B1 (en) * 2019-08-23 2021-02-09 Raytheon Technologies Corporation Gas turbine engine and method for operating same

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6991425B2 (en) 2003-09-12 2006-01-31 Honeywell International, Inc. Air turbine starter with unitary inlet and stator
WO2005042948A2 (fr) * 2003-09-12 2005-05-12 Honeywell International Inc. Lanceur de turbine a air avec admission unitaire et stator
GB0415376D0 (en) * 2004-07-09 2004-08-11 Rolls Royce Plc A turbine engine arrangement
FR2878287B1 (fr) * 2004-11-25 2009-05-22 Snecma Moteurs Sa Turboreacteur double corps double flux avec generateur de courant electrique arriere
NL2000189C2 (nl) * 2006-08-18 2008-02-19 Micro Turbine Technology B V Reactieturbine met generator.
DE102006041325A1 (de) * 2006-09-01 2008-03-06 Rolls-Royce Deutschland Ltd & Co Kg Generator-Starter-System für ein Mehrwellentriebwerk
FR2919442B1 (fr) 2007-07-27 2011-01-07 Ge Energy Products France Snc Volant d'inertie a lancement progressif.
KR100774568B1 (ko) * 2007-09-10 2007-11-08 황창성 유압식 터빈밸브 제어장치
GB0806898D0 (en) * 2008-04-16 2008-05-21 Turbine Developments Ni Ltd A combustion chamber cooling method and system
IT1399882B1 (it) * 2010-05-14 2013-05-09 Nuova Pignone S R L Turboespansore per sistemi di generazione di potenza
US9151180B2 (en) * 2010-06-15 2015-10-06 Hamilton Sundstrand Corporation Lubrication driven gas turbine engine actuation system
JP5716352B2 (ja) * 2010-10-29 2015-05-13 いすゞ自動車株式会社 ターボ過給システム
GB201102772D0 (en) 2011-02-17 2011-03-30 Rolls Royce Goodrich Engine Control Systems Ltd Pumping arrangement
JP5941744B2 (ja) * 2012-04-27 2016-06-29 株式会社Ihiエアロスペース 発電システム
US20140026871A1 (en) * 2012-07-27 2014-01-30 Gary Haven Supercharger Control Device
ITFI20120161A1 (it) * 2012-08-03 2014-02-04 Nuovo Pignone Srl "dual-end drive gas turbine"
GB201407743D0 (en) 2014-05-02 2014-06-18 Rolls Royce Plc Gas turbine engine fuel system
JP6580866B2 (ja) * 2015-05-29 2019-09-25 Ntn株式会社 エアタービン駆動スピンドル
US10011283B2 (en) * 2016-06-28 2018-07-03 Ford Global Technologies, Llc System and method for driving vehicle accessories
US20180050812A1 (en) * 2016-08-16 2018-02-22 Hamilton Sundstrand Corporation Aircraft fuel pump systems
US10914242B2 (en) * 2017-11-28 2021-02-09 Raytheon Technologies Corporation Complex air supply system for gas turbine engine and associated aircraft
RU2727655C2 (ru) * 2018-06-13 2020-07-22 Никита Владимирович Гусев Малоразмерный газотурбинный двигатель
EP4023872A4 (fr) * 2019-08-30 2023-08-30 Kawasaki Jukogyo Kabushiki Kaisha Moteur à turbine à gaz
WO2021039903A1 (fr) 2019-08-30 2021-03-04 川崎重工業株式会社 Moteur à turbine à gaz
JP2021127731A (ja) 2020-02-14 2021-09-02 川崎重工業株式会社 ガスタービンエンジン
JP7455706B2 (ja) 2020-09-04 2024-03-26 三菱重工業株式会社 ポンプ装置

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2939017A (en) * 1949-07-14 1960-05-31 Bendix Aviat Corp Air driven power supply
US2949731A (en) * 1957-05-20 1960-08-23 Standard Motor Co Ltd Gas turbine power plant
US3274757A (en) * 1963-05-16 1966-09-27 Neu Sa Combination gas turbine and dust separator
US4729218A (en) * 1985-08-08 1988-03-08 Kloeckner-Humboldt-Deutz Ag Gas turbine engine with generator arrangement
US5285626A (en) * 1992-03-20 1994-02-15 Woodward Governor Company Drive for main engine auxiliaries for an aircraft gas turbine engine
EP0694472A1 (fr) 1994-07-30 1996-01-31 Michael John Dr. Provost Moteur à turbine à gaz auxiliaire
US5577385A (en) 1995-09-11 1996-11-26 Kapich; Davorin D. Electropneumatic engine supercharger system
US5899085A (en) 1997-08-01 1999-05-04 Mcdonnell Douglas Corporation Integrated air conditioning and power unit
US6145314A (en) 1998-09-14 2000-11-14 Turbodyne Systems, Inc. Compressor wheels and magnet assemblies for internal combustion engine supercharging devices

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4503666A (en) * 1983-05-16 1985-03-12 Rockwell International Corporation Aircraft environmental control system with auxiliary power output

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2939017A (en) * 1949-07-14 1960-05-31 Bendix Aviat Corp Air driven power supply
US2949731A (en) * 1957-05-20 1960-08-23 Standard Motor Co Ltd Gas turbine power plant
US3274757A (en) * 1963-05-16 1966-09-27 Neu Sa Combination gas turbine and dust separator
US4729218A (en) * 1985-08-08 1988-03-08 Kloeckner-Humboldt-Deutz Ag Gas turbine engine with generator arrangement
US5285626A (en) * 1992-03-20 1994-02-15 Woodward Governor Company Drive for main engine auxiliaries for an aircraft gas turbine engine
EP0694472A1 (fr) 1994-07-30 1996-01-31 Michael John Dr. Provost Moteur à turbine à gaz auxiliaire
US5577385A (en) 1995-09-11 1996-11-26 Kapich; Davorin D. Electropneumatic engine supercharger system
US5899085A (en) 1997-08-01 1999-05-04 Mcdonnell Douglas Corporation Integrated air conditioning and power unit
US6145314A (en) 1998-09-14 2000-11-14 Turbodyne Systems, Inc. Compressor wheels and magnet assemblies for internal combustion engine supercharging devices

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060137355A1 (en) * 2004-12-27 2006-06-29 Pratt & Whitney Canada Corp. Fan driven emergency generator
US20100237619A1 (en) * 2006-09-12 2010-09-23 Josef Pozivil Power recovery machine
US8421258B2 (en) 2006-09-12 2013-04-16 Cryostar Sas Power recovery machine
US20100003148A1 (en) * 2007-07-30 2010-01-07 Hispano Suiza Assistance and emergency backup for the electrical drive of a fuel pump in a turbine engine
US7895819B2 (en) * 2007-07-30 2011-03-01 Hispano Suiza Assistance and emergency backup for the electrical drive of a fuel pump in a turbine engine
US20110181050A1 (en) * 2007-08-22 2011-07-28 General Electric Company Combustion turbine cooling media supply method
US20120047906A1 (en) * 2007-08-22 2012-03-01 General Electric Company Combustion turbine cooling media supply method
US20110303390A1 (en) * 2010-06-14 2011-12-15 Vykson Limited Combustion Chamber Cooling Method and System
US8519555B2 (en) 2010-11-29 2013-08-27 Pratt & Whitney Canada Corp. Combination low spool generator and ram air turbine generator
US20160053691A1 (en) * 2014-08-22 2016-02-25 Rolls-Royce Corporation Gas turbine engine system
US10125692B2 (en) * 2014-08-22 2018-11-13 Rolls-Royce Corporation Gas turbine engine system having a disengageable electric machine
US20180030900A1 (en) * 2016-08-01 2018-02-01 Honeywell International Inc. Air Turbine Starter with Integrated Motor for Main Engine Cooling
US20180093760A1 (en) * 2016-10-05 2018-04-05 Sikorsky Aircraft Corporation Flight control pump systems
US10914234B1 (en) * 2019-08-23 2021-02-09 Raytheon Technologies Corporation Gas turbine engine and method for operating same
US20210054784A1 (en) * 2019-08-23 2021-02-25 United Technologies Corporation Gas turbine engine and method for operating same
US11428161B2 (en) 2019-08-23 2022-08-30 Raytheon Technologies Corporation Gas turbine engine and method for operating same

Also Published As

Publication number Publication date
RU2003122558A (ru) 2005-01-10
FR2842564B1 (fr) 2006-01-21
RU2321761C2 (ru) 2008-04-10
CA2434492C (fr) 2011-05-31
FR2842564A1 (fr) 2004-01-23
JP4115902B2 (ja) 2008-07-09
US20040011018A1 (en) 2004-01-22
CA2434492A1 (fr) 2004-01-17
DE60304135D1 (de) 2006-05-11
DE60304135T2 (de) 2007-03-08
UA79084C2 (uk) 2007-05-25
EP1382817B1 (fr) 2006-03-22
EP1382817A1 (fr) 2004-01-21
JP2004132359A (ja) 2004-04-30

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Free format text: CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME;ASSIGNOR:SNECMA;REEL/FRAME:046939/0336

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